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-rw-r--r--uav_model.m95
1 files changed, 92 insertions, 3 deletions
diff --git a/uav_model.m b/uav_model.m
index ce7cddb..747f1b7 100644
--- a/uav_model.m
+++ b/uav_model.m
@@ -1,6 +1,30 @@
-% Copyright (C) 2024, Naoki Sean Pross, ETH Zürich
+% Compute models for Ducted Fan VTOL micro-UAV for given set of parameters.
%
-% Compute model for UAV for given set of parameters.
+% Copyright (C) 2024, Naoki Sean Pross, ETH Zürich.
+% This function generates three models:
+%
+% * A non-linear symbolic model (cannot be used directly).
+% * A linear model obtained by linearizing the the non linear model at an
+% operating point specified in the params struct argument.
+% * A uncertain linear model built atop of the linear model using SIMULINK.
+% The uncertain model contains the performance and weighting transfer
+% function given in the arguments perf and params, and is stored in the
+% SIMULINK fil euav_model_uncertain.xls.
+%
+% [MODEL] = UAV_MODEL(PARAMS, PERF, UNCERT)
+%
+% Arguments:
+% PARAMS Struct of design parameters and constants generated from uav_params
+% PERF Struct with transfer functions that describe performance
+% requirements (used for uncertain model).
+% UNCERT Struct with weighting transfer functions for the uncertainty
+% blocks (used for uncertain model).
+%
+% Return value:
+% MODEL Struct with models
+%
+% See also UAV_PARAMS
+
function [model] = uav_model(params, perf, uncert)
@@ -210,6 +234,7 @@ model.linear = struct(...
% ------------------------------------------------------------------------
% Check properties of linearized model
+
eigvals = eig(A);
% Check system controllability / stabilizability
@@ -269,6 +294,7 @@ end
h = load_system('uav_model_uncertain');
hws = get_param('uav_model_uncertain', 'modelworkspace');
+hws.assignin('params', params);
hws.assignin('model', model);
hws.assignin('perf', perf);
hws.assignin('uncert', uncert);
@@ -279,9 +305,72 @@ usys = ss(ulmod.a, ulmod.b, ulmod.c, ulmod.d);
% Save uncertain model
model.uncertain = struct(...
- 'Simulink', ulmod, ...
+ 'Simulink', ulmod, ...
'StateSpace', usys ...
);
+% The uncertain system is partitioned into the following matrix
+%
+% [ z ] [ A B_w B_u ] [ v ]
+% [ e ] = [ C_e D_ew D_eu ] [ w ]
+% [ y ] [ C_y D_yw D_yu ] [ u ]
+%
+% Struct below provides indices for inputs and outputs of partitioning.
+% Check for correctness of these values by inspecting:
+%
+% - model.uncertain.Simulink.InputName(model.uncertain.index.InputX)
+% - model.uncertain.Simulink.OutputName(model.uncertain.index.OutputX)
+%
+% Function make_idx(start, size) is defined below.
+model.uncertain.index = struct(...
+ 'InputUncertain', make_idx( 1, 17), ... % 'v' inputs
+ 'InputDisturbance', make_idx(18, 12), ... % 'w' inputs for noise
+ 'InputReference', make_idx(30, 12), ... % 'w' inputs for reference
+ 'InputNominal', make_idx(42, 5), ... % 'u' inputs
+ 'OutputUncertain', make_idx( 1, 17), ... % 'z' outputs
+ 'OutputError', make_idx(18, 17), ... % 'e' outputs
+ 'OutputNominal', make_idx(35, 12) ... % 'y' outputs
+);
+
+% ------------------------------------------------------------------------
+% Check properties of uncertain model
+
+% % Check that (A, B_u, C_y) is stabilizable and detectable
+% A = model.uncertain.StateSpace(...
+% model.uncertain.index.OutputUncertain, ...
+% model.uncertain.index.InputUncertain ...
+% );
+%
+% B_u = model.uncertain.StateSpace(...
+% model.uncertain.index.OutputUncertain, ...
+% model.uncertain.index.InputNominal ...
+% );
+%
+% % TODO: do PBH test
+%
+% % Check that D_eu and D_yw are full rank
+% D_eu = model.uncertain.StateSpace(...
+% model.uncertain.index.OutputError, ...
+% model.uncertain.index.InputNominal ...
+% );
+%
+% D_yw = model.uncertain.StateSpace(...
+% model.uncertain.index.OutputNominal, ...
+% model.uncertain.index.InputDisturbance ...
+% );
+
+% if rank(D_eu) < min(size(D_eu))
+% fprintf('D_eu is not full rank!\n')
+% end
+%
+% if rank(D_yw) < min(size(D_yw))
+% fprintf('D_yw is not full rank!\n')
+% end
+
+end
+
+function [indices] = make_idx(start, size)
+ indices = [start:(start + size - 1)]';
end
+
% vim: ts=2 sw=2 et: